Dynamic Behavior Analysis of Intermediate Bearing-Squeeze Film Dampers-Rotor System under Constant Maneuvering Overload

Figure 11

Variation result of the static displacements of disk 3 with overload under maneuver flight conditions. (a) Horizontal magnitude, numerical simulation. (b) Horizontal magnitude, experimental results. (c) Vertical magnitude, numerical simulation. (d) Vertical magnitude, experimental results.

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